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Development of BEM for ceramic compositesBEST-CMS (boundary element solution technology - composite modeling system) is an advanced engineering system for the micro-analysis of fiber composite structures. BEST-CMS is based upon the boundary element program BEST3D which was developed for NASA by Pratt and Whitney Aircraft and the State University of New York at Buffalo under contract NAS3-23697. BEST-CMS presently has the capabilities for elastostatic analysis, steady-state and transient heat transfer analysis, steady-state and transient concurrent thermoelastic analysis, and elastoplastic and creep analysis. The fibers are assumed to be perfectly bonded to the composite matrix, or in the case of static or steady-state analysis, the fibers may be assumed to have spring connections, thermal resistance, and/or frictional sliding between the fibers and the composite matrix. The primary objective of this user's manual is to provide an overview of all BEST-CMS capabilities, along with detailed descriptions of the input data requirements. In the next chapter, a brief review of the theoretical background is presented for each analysis category. Then, chapter three discusses the key aspects of the numerical implementation, while chapter four provides a tutorial for the beginning BEST-CMS user. The heart of the manual, however, is in chapter five, where a complete description of all data input items is provided. Within this chapter, the individual entries are grouped on a functional basis for a more coherent presentation. Chapter six includes sample problems and should be of considerable assistance to the novice. Chapter seven includes capsules of a number of fiber-composite analysis problems that have been solved using BEST-CMS. This chapter is primarily descriptive in nature and is intended merely to illustrate the level of analysis that is possible within the present BEST-CMS system. Chapter eight contains a detail description of the BEST-CMS Neutral File which is helpful in writing an interface between BEST-CMS and any graphic post-processor program. Finally, all pertinent references are listed in chapter nine.
Document ID
19940017304
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Henry, D. P.
(Calspan-State Univ. of New York Joint Venture Buffalo, NY, United States)
Banerjee, P. K.
(Calspan-State Univ. of New York Joint Venture Buffalo, NY, United States)
Dargush, G. F.
(Calspan-State Univ. of New York Joint Venture Buffalo, NY, United States)
Hopkins, D. A.
(NASA Lewis Research Center Cleveland, OH., United States)
Goldberg, R. K.
(NASA Lewis Research Center Cleveland, OH., United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1993
Subject Category
Composite Materials
Report/Patent Number
NAS 1.26:194718
NASA-CR-194718
Report Number: NAS 1.26:194718
Report Number: NASA-CR-194718
Accession Number
94N21777
Funding Number(s)
CONTRACT_GRANT: NAG3-888
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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